Boeing 767-300

Service difficulty reports · 2,161

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '767300'
  ORDER BY difficulty_date DESC"

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SDR HALA0600680Pressure Switch · unknownETOPS SIGNIFICANT SYSTEM, LOW PRESS LIGHT ILLUM EICAS MSG DISPLAYED C HYD PRIM1. EICAS MSG C HYD SYS MAINT WAS NOT DISPLAYED. OPS CK CENTER HYD SYS COULD NOT DUPLICATE PROBLEM. REPLACED C1 ELECTRIC HYD PUMP PRESSURE SWITCH IAW MM 29-11-18. OPS AND LEAK CK OK Sep 7, 2006 · N594HA · Boeing 767300 · Hydraulic System, MainSDR HALA0600674Vent Line · damagedETOPS SIGNIFICANT SYSTEM, FOUND HOLE IN NR 3 BEARING OIL VENT TUBE ON NR 2 ENGINE. REMOVED TUBE FOR EVALUATION, REMOVED AND REPLACED LINE PER POWERPLANT BUILD UP MANUAL , MM CHAP 71-00-00 LINE SECURED AND SAFETIED. LEAK CHECKED GOOD.Sep 7, 2006 · N581HA · Boeing 767300 · Engine Oil Storage (Airframe Furnished)SDR HALA0600672Panel · openBTB -WHILE TAXING OUT ROW 29 CEG, O2 PANEL FELL OUT, RTN TO GATE FOR MNT.//RESET DOOR LATCH PER AMM 35-21-15 SECURITY GOOD.Sep 6, 2006 · N594HA · Boeing 767300 · Passenger Oxygen SystemSDR HALA0600667Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - RT ENG EEC MODE AMBER EICAS MSG CAME ON NEAR TOP OF CLIMB. SUCCESSFUL RESET FOLLOWING QRH PROCEDURE. T/S PER FIM 73-21-00, FOUND P5 LINE FAULT CHA/B ON PIMU. INSPECTED PHEUMATIC LINES P5 AND P2, NO DISCREPANCIES FOUND. CLEARED PISep 6, 2006 · N581HA · Boeing 767300 · Engine Temperature Indicating SystemSDR HALA0600666Warning Message · false activationETOPS SIGNIFICANT SYSTEM - `RUDDER RATIO` MAINTENANCE MESSAGE ON ECS/MSG EICAS PAGE. DID BITE CHECK FOR LT/RT RUDDER RATIO CONTROL/MODULE BOXES IN E&E COMPARTMENT. NO FAULTS FOUND, RESET C/W ON BOTH LT & RT BOXES MESSAGE CLEARED.Sep 6, 2006 · N580HA · Boeing 767300 · Central WarningSDR HALA0600768Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 8, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 PER SRM 53-00-01-2R-8, SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600759Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1074 BETWEEN 3R AND 4R. DRILLED OUT DAMAGE O A DIA OF .127 INCH PER SRM 03-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFCL INSPECTED REWORK AREA IAW D634T301, PT6, 51-00-16, NO CSep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HAL0600763Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1133 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8, SEC1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.8. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,51-00-Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600761Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1110 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO DIA OF .128 INCH PER SRM 53-00-01-2R-8, SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-8. REWORK AREA IAW D634T301, PT6, 51-00-16, NO CRACKS NOTESep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600763Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1133, BETWEEN STR 5R AND STR 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600764Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1145 BETWEEN STR 5R AND STR 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP NO CRACKS NOTED IAW 767 NDT, PT6 51-00-19. Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600769Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 27, BETWEEN STR 7R & STR. 8R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SRC1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PTSep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600767Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1192, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600770Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 +38. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS FREE OF CRACKS, PER STEP 3,B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767NDT, PT6, 51-00-19. QC VERISep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600772Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 86, BETWEEN STR 8R AND STR 9R. DRILLED OUT DAMAGE TO A DIA OF .128 INCH PER SRM 53-00-01/201 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, 51-00-19Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600771Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 +78, BETWEEN STR 8R AND STR 9R. DRILL OUT DAMAGE TO A DIA OF .128 INCH PER SRM 53-00-01/201 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS FREE OF CRACKS. HFEC INSP OF HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,51-00Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600766Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1183, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 INCH PER SRM 53-00-01-2R-9 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B.HFEC INSP. HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600760Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1096, BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF.185 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSPECTED REWORK AREA IAW D634T301 PT6 51-00-16, NOSep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600765Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1155 BETWEEN STR 6R AND 7R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, 51-0Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600762Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1126 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8, SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT PT6, 51-00-Sep 5, 2006 · N597HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600668Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE SLOW TO START STARTER CUT OUT AT APPROX 47%, 130 SECONDS FROM FUEL ON TO IDLE SPEED. RAN NR 2 ENGINE ON GROUND, STARTER CUTOUT AT 49%, 85 SEC FROM FUEL ONTO IDLE SPEED. OK TO CONTINUE PER HAL M105 FILE 584060.Sep 5, 2006 · N584HA · Boeing 767300 · Engine StarterSDR HALA0600665Indication Sys · erraticETOPS SIGNIFICANT SYSTEM - NR 2 EGT ERRATIC AND FLUCTUATING BETWEEN 750-350 ON CLIMBOUT FOR APPROX 2 MINS, THAN STABLE. ACCOMPLISHED FIM 77-21-00 FIG 103, NO FAULTS OR DAMAGE. CHECKED ENG WIRING PER WDM 77-21-11 AND SSM 77-00-01 SHOOK HARNESS, NO FLUCTUATIONSep 5, 2006 · N594HA · Boeing 767300 · Engine Temperature Indicating SystemSDR HALA0600664Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ICAS MSG R ENG EEC MODE DISPLAYED, SYS WAS SUCCESSFULLY RESET. T/S PER FIM 73-21-00 FIG 113, NO MSG IN PIMU CLEARED MTC MSG RUN ENG PER FIM PIMU INDEX 350-22. MSG DID NOT RETURN, SYS OK.Sep 5, 2006 · N581HA · Boeing 767300 · Central WarningSDR HALA0600670Hydraulic System · unknownETOPS SIGNIFICANT SYSTEM - DURING CLIMBOUT DURING THE LAST 10,000FT OF CLIMB L ENG PRIMARY HYD PRESS LIGHT CAME ON FOLLOWED BY THE L ELECT DEMAND PRESS LT. CREW NOTED PRESS WOULD DROP TO APPX 1700 PSI, RTN TO NORMAL & PRESS LIGHT WENT OUT. HYD QUANTITY 1.4 ISep 4, 2006 · N591HA · Boeing 767300 · Hydraulic System, MainSDR HALA0600669Idg · malfunctionedETOPS SIGNIFICANT SYSTEM - ON BASE LEG LANDING IN HNL RECEIVED L GEN OFF LIGHT & BOTH UTILITY BUSS OFF LIGHTS. STARTED THE APU, LANDED THEN RESET GEN CONT SWITCH. CONDITION RETURNED TO NORMAL. PERFORMED BPCU BITE PROCEDURE PER FIM 24-20-00-MSG FOR LT SYS ARSep 4, 2006 · N591HA · Boeing 767300 · Alternator-Generator DriveSDR HALA0600671Status Message · false activationETOPS SIGNIFICANT SYSTEM - WXR SYS STATUS LIGHT CAME ON. RADAR OPS NORMAL. RESET WEATHER RADAR SYSTEM. OPS GOOD CHECK PER M/M 34-43-00.Sep 4, 2006 · N591HA · Boeing 767300 · Weather Radar SystemSDR HALA0600653Eec · faultedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE EEC MODE EICAS MESSAGE DISPLAYED. T/S PER FIM 73-21-00 FIG 113 PIMU FAULTED EEC CHANNEL A/B P2 AND P5 LINE. INSPECTED P2 AND P5 LINES PER FIM 350-21. NO FAULTS NOTED. CLEARED PIMU AND RAN ENG NR 2 TO 1.4 EPR. CONFIRSep 4, 2006 · N581HA · Boeing 767300 · Fuel Controlling SystemSDR NOCA12906Blades · bird strikeBIRD STIRKE ON TAKE OFF FROM BJL RT ENGINE, FAN VIB 4.1 RECORDED. LANDED SAFELY AT BJL AFTER FUEL DUMPED. REPLACED 4 FAN BALDES, OPS NORMAL.Sep 3, 2006 · N768NA · Boeing 767300 · Turbine Engine Compressor SectionSDR HALA0600656Wire · damagedETOPS SIGNIFICANT SYSTEM - CALLS ON ANY RADIO FAILED TO DISPLAY SELCAL MESSAGE AND SOUND CHIME. REPAIRED WIRING TO SELCAL CODING OPS CHECK OK PER AMM 23-21-00.Sep 3, 2006 · N594HA · Boeing 767300 · Communications System WiringSDR HALA0600655Warning Light · illuminatedETOPS SIGNIFICANT SYSTEM - (LOWER EICAS) STATUS MSG -WXR SYS-. BOTH LEFT & RIGHT WX RADAR SYSTEMS OPS CHECK OK PER AMM 34-43-00. NO FAULTS FOUND.Sep 3, 2006 · N581HA · Boeing 767300 · Weather Radar SystemSDR HALA0600657Wire · failedETOPS SIGNIFICANT SYSTEM - BOTH FMCS FAIL WHEN RIGHT EFI SWITCH SELECTED TO ALTN. REPAIRED WIRING TO RELAY K2070 FMC NR 1 & NR 2, OPS CHECK OK PER AMM 34-61-00. EFIS SYSTEM OPS CHECK OK PER AMM 34-22-00.Sep 3, 2006 · N594HA · Boeing 767300 · Navigation System WiringSDR HALA0600688Support Bracket · crackedLT WING T/E WS 530 LWR T/E PANEL SUPPORT BRACKET CRACKED IN RADUS OB SIDE OF IB AILERON OB SUPPORT FITTING. ACCESSED LOWER T/E PANEL FASTENERS AND REMOVED CRACKED BRACKET JUST OB OF AILERON SUPPORT FITTING. FABRICATED REPLACEMENT BRACKET FROM 7075-0 BARE SHEESep 1, 2006 · N597HA · Boeing 767300 · Wing Miscellaneous StructureSDR HALA0600654Shutoff Valve · failedBTB - NR 1 ENGINE NO BLEED AIR. T/S PER FIM - PNEUMATIC SUPPLY BITE MODULE FAULTED LEFT ENG PRSOV. REMOVED AND REPLACED LEFT ENG PRSOV PER M/M 36-11-09. ALSO REPLACED LEFT ENG BLEED SUPPLY CONTROL CARD IN P50 PANEL PER MM 36-11-12. RAN ENGINE AND PRSOV OP Sep 1, 2006 · N590HA · Boeing 767300 · Pneumatic Distribution SystemSDR HALA0600719Support · damagedRT WING T/E, AFT PANEL SUPPORT FOR PNL NR 661 IB AFT L ANGLE HAS A FIGURE 8 HOLE AND LWR FASTENER LOOSE. REMOVED, FABRICATED NEW AND INSTALLED L ANGLE RT WING T/E AFT PANEL SUPPORT IAW OHM 20-50-01-06-0, MM 51-21-00-377-001.Aug 31, 2006 · N597HA · Boeing 767300 · Wing Miscellaneous StructureSDR HALA0600718Channel · crackedR/W CRACKED CHANNEL IB END OB FLAP 7 INCHES FROM L/E OF CLOSE OUT PANEL. REMOVED CRACKED CHANNEL FROM R/W IB END OF OB FLAP IAW SRM 51-40-02.REPAIRED CHANNEL IAW SRM 51-70-11 FIG 1 STEPS 1-12. REPAIRED DOUBLER MATERIAL 2024-T3 .63 INCHES, LOT NR 709033. INSTAAug 31, 2006 · N597HA · Boeing 767300 · Trailing Edge FlapsSDR HALA0600687Crank Assy · chafedR/W OB FLAP ACTUATOR CRANK ARM 6-9 LINK LWR OB SIDE CHAFING ON LINK SUPPORT FITTING AT FWD OB SIDE. REPAIRED CHAFED AREA ON LINK SUPPOR AND 6-9 LINK IAW SRM 57-53-02 AND SRM 51-20-06.Aug 31, 2006 · N597HA · Boeing 767300 · Aileron TabsSDR UPS06647908Brake · leakingINSPECTION TYPE: ETOP RT HYDRAULIC QTY ZERO; EICAS MSG RT HYD QTY DISPLAYED. SYSTEM PRESSURE LIGHT NOT ILLUM. NOTED AFTER EXITING RUNWAY ON LANDING. FOUND DAMAGE TO NR 8 BRAKE (RT AFT OB). THIS FLIGHT INVOLVED A BRAKE ROTOR FAILURE LEADING TO THE COMPLETE LOSAug 31, 2006 · N310UP · Boeing 767300 · Landing Gear Brake SystemSDR HALA0600717Rib · crackedANGLE CRACKED IN FIXED L/E FWD OF RIB ON OB SIDE OF NR 8 SLAT, OB ROTARY ACTUATOR. REMOVED ANGLE IN L/E OB NR 8 ROTARY ACTUATOR, REPLACED ANGLE AND INSTALLED ALL BUT (3) RIVETS, COMMON TO SKIN IAW SRM 51-40-01. INSTALLED (3) FASTNERS COMMON TO L/E SKIN IAW SAug 30, 2006 · N597HA · Boeing 767300 · Leading Edge DevicesSDR UPS06647836Servo · malfunctionedUNCOMMANDED RUDDER YAW TWICE IN FLIGHT. R & R LT & RT YAW DAMPER SERVO IAW MM 22-21-02-4. LEAK CHECK RIGHT & LEFT YAW DAMPER SERVO PER TECH SERVICES. R&R RIGHT YAW DAMPER MODULE ASSY IAW MM 22-21-04-2. ALSO R&R LEFT YAW DAMPER MODULE ASSY AS PRECAUTIONARY. PAug 30, 2006 · N306UP · Boeing 767300 · Rudder Control SystemSDR HALA0600643Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, EICAS STATUS MESSAGE "ELEVATOR FEEL" DISPLAYED. ACCOMPLISHED FIM 27-30-00 FIG 106, NO DEFECTS NOTED.Aug 30, 2006 · N591HA · Boeing 767300 · Elevator Control SystemSDR HALA0600646Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, APU BITE BITE EICAS MTC MSG FOUND ON OVERNIGHT CHECK. PERFORMED APU ECU BITE PER FIM 49-11-00/101 FIG 103, NO FAULTS ERASED. MSG ON EICAS ECS MSG PAGE DID NOT RETURN.Aug 30, 2006 · N583HA · Boeing 767300 · APU Indicating SystemSDR HALA0600645Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, L ENG FIRE LP2 STATUS MSG FOUND ON OVERNIGHT CHECK. PERFORMED TEST PER FIM 26-11-00/101 FIG 104, NO FAULTS FOUND MSGV DID NOT RETURN.Aug 30, 2006 · N583HA · Boeing 767300 · Fire DetectionSDR HALA0600647Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM, FMC DISPLAYED ON EICAS WITH NO CORRESPONDING FMS MESSAGE. NO EICAS MESSAGE "FMC" DISPLAYED ON ARRIVAL. OPS CHECK OK PER MM 34-61-00.Aug 30, 2006 · N588HA · Boeing 767300 · Central WarningSDR HALA0600747Keelbeam · corrodedCORROSION ON KEELBEAM SURFACE, BS 970, RBL 8. REMOVED CORROSION ON KEEL BEAM OF BS 970 RBL 8 IN AN AREAS OF 2.5 X 1.5 X .035 INCH FROM ORIGINAL THICKNESS OF .360 INCH. FOUND BLENDED AREA TO BE IN LIMITS PER SRM 53-50-12 FIGURE 101.Aug 29, 2006 · N597HA · Boeing 767300 · Fuselage Main, KeelSDR HALA0600642A/C Pack · inoperativeETOPS SIGNIFICANT SYSTEM - R PACK INOP LT ON DURING DESCENT. R PACK BITE MSG ON MAINT MESSAGE DISPLAYED ON EICAS. PERFORMED FIM 21-51-00 FIG 103. RT PACK TEMP CONT INDICATED TEMP VALVE FAULT. CLEANED CONNECTOR ON VALVE. RT PACK OPS NORMAL PER FIM 21-51-00Aug 29, 2006 · N584HA · Boeing 767300 · Cabin Cooling SystemSDR HALA0600639Control Column · disconnectedBTB -COLUMN DISC- ALERT MSG CAME ON DURING TAXI. PERFORMED FIM 27-30-00 AND COLUMN WAS PHYSICALLY DISCONNECTED. RECONNECTED CONTROL COLUMN PER AMM 27-31-10, OPS CHECK GOOD, MSG CLEARED.Aug 29, 2006 · N476HA · Boeing 767300 · Control Column SectionSDR HALA0600686Seal · damagedBLADE SEAL DAMAGED ON LEADING EDGE ON NR 2 ENGINE PYLON PANEL NR 441AT. REMOVED RIVETS FROM NR 2 ENG PYLON PANEL NR 441 AT BLADE SEAL IAW SRM 51-40-02.Aug 28, 2006 · N597HA · Boeing 767300 · Nacelle/Pylon Miscellaneous StructureSDR HALA0600685Attach Fitting · crackedIB T-CLIP IS CRACKED ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY, NAS STATION 308. REMOVED AND REPLACED T-CLIP ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY NAC, STA 308. IAW SRM 51-40-02.Aug 28, 2006 · N597HA · Boeing 767300 · Nacelle/Pylon Miscellaneous StructureSDR HALA0600635Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - ELEV FELL LIGHT ILLUMINATED DURING APPROACH WITH ELEV FELL EICAS MESSAGE. ACCOMPLISHED FIM 27-30-06 FIG 106, NO DEFECTS NOTED, SYS TEST OK.Aug 28, 2006 · N591HA · Boeing 767300 · Elevator Control SystemSDR HALA0600633Skin · scratchedON WALKAROUND FOUND SCRATCH 30 INCHES BELOW AFT EDGE OF L-4 DOOR. BLENDED AREA, PERFORMED FLOOR PENETRANT TEST, NO CRACKS NOTED. TREATED, PRIMED & PAINTED AREAS PER SRM. DAMAGE OF SCRATCH WITHIN LIMITS PER SRM 53-00-01/101, SILVER DOT INSTALLED. OK FOR SERAug 27, 2006 · N580HA · Boeing 767300 · Fuselage Main, Plate/Skin
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